WO2006113041A3 - Multi-ring system for fuselage barrel formation - Google Patents

Multi-ring system for fuselage barrel formation Download PDF

Info

Publication number
WO2006113041A3
WO2006113041A3 PCT/US2006/010705 US2006010705W WO2006113041A3 WO 2006113041 A3 WO2006113041 A3 WO 2006113041A3 US 2006010705 W US2006010705 W US 2006010705W WO 2006113041 A3 WO2006113041 A3 WO 2006113041A3
Authority
WO
WIPO (PCT)
Prior art keywords
mold
fuselage barrel
fuselage
support structure
ring system
Prior art date
Application number
PCT/US2006/010705
Other languages
French (fr)
Other versions
WO2006113041A2 (en
Inventor
Branko Sarh
Original Assignee
Boeing Co
Branko Sarh
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Boeing Co, Branko Sarh filed Critical Boeing Co
Priority to CA2604079A priority Critical patent/CA2604079C/en
Priority to EP06758186A priority patent/EP1874621A2/en
Publication of WO2006113041A2 publication Critical patent/WO2006113041A2/en
Publication of WO2006113041A3 publication Critical patent/WO2006113041A3/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/32—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core on a rotating mould, former or core
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061—Frames
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/064—Stringers; Longerons
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2211/00—Modular constructions of airplanes or helicopters
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Abstract

An aircraft fuselage barrel (10) includes a skin (12) and a shear tie (18). The shear tie (18) resides within and is integrally formed with the skin (12). The shear tie (18) is separate from and configured for frame attachment thereon. A multi-ring system (79) for fuselage barrel formation includes a mold (68) with a ring (50). The ring (50) has width (W2) approximately equal to a separation distance (D) between two adjacent fuselage frames (22) and includes a module (52) that has a circumferential length (L1) that is greater than a circumferential distance between two fuselage longerons (14). A support structure (80) is coupled to and supports the mold (68). A method of forming the aircraft fuselage barrel (10) includes constructing the support structure (80). Rings (86) of the mold (68) are attached to and over the support structure (80). The mold (68) is constructed. Material is laid-up onto the mold (68) to integrally form the one-piece fuselage barrel (10) including a Hat-configured longeron (14).
PCT/US2006/010705 2005-04-13 2006-03-22 Multi-ring system for fuselage barrel formation WO2006113041A2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CA2604079A CA2604079C (en) 2005-04-13 2006-03-22 Multi-ring system for fuselage barrel formation
EP06758186A EP1874621A2 (en) 2005-04-13 2006-03-22 Multi-ring system for fuselage barrel formation

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/907,729 2005-04-13
US10/907,729 US7410352B2 (en) 2005-04-13 2005-04-13 Multi-ring system for fuselage barrel formation

Publications (2)

Publication Number Publication Date
WO2006113041A2 WO2006113041A2 (en) 2006-10-26
WO2006113041A3 true WO2006113041A3 (en) 2007-04-05

Family

ID=36781543

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2006/010705 WO2006113041A2 (en) 2005-04-13 2006-03-22 Multi-ring system for fuselage barrel formation

Country Status (5)

Country Link
US (3) US7410352B2 (en)
EP (2) EP2177435B1 (en)
CA (3) CA2857925C (en)
ES (1) ES2388131T3 (en)
WO (1) WO2006113041A2 (en)

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Also Published As

Publication number Publication date
US8173055B2 (en) 2012-05-08
CA2604079C (en) 2014-05-06
WO2006113041A2 (en) 2006-10-26
CA2604079A1 (en) 2006-10-26
US20080149768A1 (en) 2008-06-26
EP2177435B1 (en) 2012-05-16
US7410352B2 (en) 2008-08-12
CA2843080A1 (en) 2006-10-26
EP2177435A1 (en) 2010-04-21
CA2857925C (en) 2016-09-13
CA2843080C (en) 2015-12-29
US20080237442A1 (en) 2008-10-02
EP1874621A2 (en) 2008-01-09
US20060231682A1 (en) 2006-10-19
CA2857925A1 (en) 2006-10-26
ES2388131T3 (en) 2012-10-09

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